Verfahren und System zur Steuerung eines Sequentiellen Gasturbinenmotors
Anmelder: General Electric Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3376003
- Aktenzeichen
- EP18160629
- Anmeldetag
- 8. März 2018
- Veröffentlichung
- 29. April 2020
- Erteilung
- 29. April 2020
- Rechtsraum
- EP
- IPC
- F02C6/18F01K23/10F23N1/02F23C6/04F23R3/34
Abstract
A method (90) for operating a gas turbine system (10) includes utilizing a gas turbine controller (46) to determine (94) a schedule (70) for a firing temperature for operative burners (28) of a second combustor (18) located downstream (8) of a first combustor (14) when the gas turbine system (10) is operating in a low part load mode. During the low part load mode, multiple burners (28) for the second combustor (18) are switched-off. Further, the schedule (70) is determined based on a position of inlet guide vanes (30) of a compressor (12) of the gas turbine system (10) located upstream (6) of both the first and second combustors (14, 18). The method (90) also includes controlling (96) the firing temperature of the operative burners (28) utilizing the schedule (70) during the low part load mode to keep the gas turbine system (10) within relevant operational limits of the gas turbine system (10).
Anmelder
- Firma
- General Electric Company
- Land
- 🇺🇸 USA
US-amerikanischer Technologiekonzern mit Sitz in Massachusetts. Historisch aktiv in Energieerzeugung, Luftfahrttriebwerken, Medizintechnik und Industrietechnik über verschiedene Geschäftsbereiche.
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